SLIDE 1
18TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS
1 Introduction
The rapid growth of the aviation industry coupled with rising fuel costs and concerns over the environment are keeping airframe manufacturers under pressure to improve aircraft efficiency. Lighter airframe structures offer a direct means of raising aircraft fuel efficiency thus reducing emissions and lowering operating costs. However, as aircraft structures also account for a large proportion
- f their cost, it is imperative that focus remains on
keeping manufacturing costs low. The use of composite materials has steadily increased in recent years in an effort to achieve greater weight savings in aircraft. Until recently the standard method for curing composites for primary aircraft structures has been the autoclave. Heat and pressure are applied to vacuum bagged prepreg laminates enabling high fibre volume fraction and low void content components to be produced. However, the use of autoclaves is also accompanied by apparent high costs, which stem from high acquisition and operating costs. The reduction of these operating costs is a priority for airframe manufacturers, thus stimulating the recent interest in
- ut of autoclave (OOA) processing.
The primary focus of this work is to quantify the economic and environmental differences between autoclave curing and other selected OOA processes through a comparison that assumes appropriately sized ovens and autoclaves. Key parameters affecting costs are identified along with environmentally dominant stages of the manufacturing processes.
2 Approach and methods
A case study approach is applied where production costs are estimated using technical cost modelling (TCM) and related environmental impacts are quantified with life cycle assessment (LCA). A 400 x 400 x 4 mm carbon fibre reinforced panel was chosen as a functional unit to be produced with the following 5 material/curing scenarios: Scenario 1 (Auto PP), Autoclave processing with unidirectional (UD) carbon fibre (CF) prepreg. Scenario 2 (Therm PP), Thermal oven curing with a CF OOA prepreg system. Scenario 3 (Micro PP), Microwave oven curing with a CF OOA prepreg system. Scenario 4 (Therm inf), Thermal oven curing with liquid resin infused (LRI) CF non-crimp fabric (NCF). Scenario 5 (Micro inf), Microwave oven curing liquid resin infused (LRI) CF non-crimp fabric (NCF). The ovens and autoclave chosen for the study were of comparable volume (0.79 m3 for the thermal
- ven and autoclave, 0.65 m3 for the microwave).
2.1 Cost modelling
Cost modelling is carried out using a technical
cost model developed at EPFL which is based upon an activity based costing (ABC) approach [1]. A production process is defined which contains all the relevant processes equipment and labour to produce a specific component. The process is then segmented
ASSESSING THE ECONOMIC AND ENVIRONMENTAL POTENTIAL OF OUT OF AUTOCLAVE PROCESSING
R.A. Witik1, F. Gaille2 , R. Teuscher1, H. Ringwald3 V. Michaud1, Jan-Anders Månson1
1 Laboratoire de Technologie des Composites et Polymères (LTC), Ecole Polytechnique Fédérale
de Lausanne (EPFL), CH-1015 Lausanne, Switzerland.
2 EADS Deutschland, Innovation Works, Dept LG_CT, D-81663 Munich, Germany. 3Institute of Aircraft Design, Pfaffenwaldring 31, 70569, Stuttgart.